Abstract
Studies of a proportional-integral implicit model-following control law are presented. The research focuses on the ability of the control law to recover the performance of a system with failed actuators or structural damage to its prefailure level. Properties of the implicit model-following strategy are examined, and conditions for control reconfiguration are stated. The control law is applied to the lateral-directional model of a fighter aircraft, and control restructuring is shown for changes in control and system matrices. It is concluded that the implicit model-following scheme is a good candidate for control reconfiguration.
| Original language | English (US) |
|---|---|
| Pages (from-to) | 303-309 |
| Number of pages | 7 |
| Journal | Journal of Guidance, Control, and Dynamics |
| Volume | 13 |
| Issue number | 2 |
| DOIs | |
| State | Published - Mar 1990 |
All Science Journal Classification (ASJC) codes
- Aerospace Engineering
- Applied Mathematics
- Electrical and Electronic Engineering
- Control and Systems Engineering
- Space and Planetary Science